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Minimum Performance Standard for Airborne Head Up Display (HUD)

A-4HUD Head-up Display Subcommittee
  • Aerospace Standard
  • AS8055A
  • Current
Published 2015-07-28 by SAE International in United States
This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head-Up Displays (HUDs) in fixed wing (14 CFR part 23, 25) aircraft; while this document is also applicable to rotorcraft (14 CFR part 27, 29) additional performance standards may be required for rotorcraft. This aerospace standard covers basic display standards, but does not include specific application requirements. Specific applications can include flight instrumentation, navigation, engine and system status, alerting, surveillance, communication, terrain awareness, weather, enhanced vision, synthetic vision and other displays. This document covers criteria for conformal and non-conformal HUD systems that are intended for use in the flight deck by the pilot or copilot. Display minimum performance characteristics are specified for standard and other environmental conditions for the purpose of product qualification. This document does not address sensor imaging systems, displays worn by the pilot (goggles, helmet mounted displays) or specific symbology to be displayed. This document is intended to be used in combination with other guidance material contained in current system specific, Technical Standard Orders (TSOs), Advisory Circulars (ACs), and other…
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Optical Measurement Procedures for Airborne Head Up Display (HUD)

A-4HUD Head-up Display Subcommittee
  • Aerospace Standard
  • ARP5287
  • Current
Published 2008-01-04 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne binocular Head Up Displays (HUDs). This document covers methods for conformal and non-conformal HUD systems that are intended for use in the cockpit by the pilot or copilot. The focus of this document is on displays that generate the HUD information using a cathode ray tube (CRT), however, the majority of the methods can be applied to other display technologies. These measurement methods are provided for testing to the requirements of AS8055. This document does not address measurement methods for sensor imaging systems, or displays worn by the pilot (goggles, helmet mounted displays).
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Transport Category Airplane Head Up Display (HUD) Systems

A-4HUD Head-up Display Subcommittee
  • Aerospace Standard
  • ARP5288
  • Current
Published 2008-01-04 by SAE International in United States
The material provided in this document consists of recommendations related to the design, analysis, testing, and intended functions of head up displays (HUDs) for transport category airplanes. The content of the document is limited to statements of general design and installation considerations, including display function criticality and compliance considerations; symbology, coding, clutter, dimensionality, and attention getting requirements; equipment installation; display visual characteristics; failure modes; information display and formatting; specific integrated display and mode; and system verification.
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Minimum Performance Standard for Airborne Head Up Display (HUD)

A-4HUD Head-up Display Subcommittee
  • Aerospace Standard
  • AS8055
  • Historical
Published 2008-01-04 by SAE International in United States
This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head Up Displays (HUDs) in fixed wing aircraft. This document covers criteria for conformal and non-conformal HUD systems that are intended for use in the cockpit by the pilot or copilot. Display minimum performance characteristics are specified for standard and other environmental conditions for the purpose of product qualification. This document does not address sensor imaging systems, displays worn by the pilot (goggles, helmet mounted displays) or specific symbology to be displayed.
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